Piper SENECA III User Manual

PILOT'S
OPERATING
HANDBOOK LOG OF REVISIONS
(cont)
Revision
FAA
Approval
Number
and
Revised
!
Description
of
Revision
Signature
and
Code
Pages
Date
R 6
9-82
Deleted
Note.
(PRS30923)
9-131
Added
Supplement No.
20
(cont)
thru
(Edo-Avionics
Command
Ward Evans
9- I34
Elect
ric Trim System)
Sept
23,
1983
Rev.
7
4-5
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+31.
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7-i
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Table
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7 11
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9-i
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Table of
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9-ii
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Supplement
2I.
9-9
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title.
5
.RAL
isedpla
e
;
added Supple-
thru
ment
21,
Century 31 Autopilot
Ward Evans
9-154
Installation. Feb.
10.
1984
REPORT:
VB-Ill0
vi-i

Piper SENECA III Specifications

General

Manufacturer	Piper Aircraft
Model	Seneca III
Engine Type	Piston
Engine Model	Continental TSIO-360-KB
Seating Capacity	6
Cruise Speed	188 knots (216 mph, 348 km/h)
Length	28 ft 7 in (8.71 m)
Max Takeoff Weight	4, 750 lb (2, 155 kg)
Horsepower	220 hp each
Service Ceiling	25, 000 ft (7, 620 m)
Height	9 ft 11 in (3.02 m)
Propellers	2-bladed constant speed